US20110243728A1 - Blower designed for fitting particularly in a chamber furnace - Google Patents

Blower designed for fitting particularly in a chamber furnace Download PDF

Info

Publication number
US20110243728A1
US20110243728A1 US12/662,146 US66214610A US2011243728A1 US 20110243728 A1 US20110243728 A1 US 20110243728A1 US 66214610 A US66214610 A US 66214610A US 2011243728 A1 US2011243728 A1 US 2011243728A1
Authority
US
United States
Prior art keywords
rotor wheel
diameter
inlet
blower
chamber furnace
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US12/662,146
Inventor
Radomir Magiera
Wladyslaw Krllowicz
Krzysztof Jozwik
Jozef Olejnik
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Politechnika Lodzka
Original Assignee
Seco/Warwick SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Seco/Warwick SA filed Critical Seco/Warwick SA
Priority to US12/662,146 priority Critical patent/US20110243728A1/en
Assigned to SECO/WARWICK S.A. reassignment SECO/WARWICK S.A. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: JOZWIK, KRZYSZTOF, Kryllowicz, Wladyslaw, Magiera, Radomir, OLEJNIK, JOZEF
Assigned to POLITECHNIKA LODZKA reassignment POLITECHNIKA LODZKA ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: SECO/WARWICK S.A.
Publication of US20110243728A1 publication Critical patent/US20110243728A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/30Vanes

Definitions

  • This invention relates to a blower designed for fitting in a chamber furnace in particular and used, among others, in furnaces for annealing of aluminium sheet.
  • blowers In furnaces requiring circulation of hot gases, usually radial or axial blowers are used. The fitting of the latter is subject to significant restrictions that affect their operating parameters. Due to the conditions of the bearings operation, the blowers are usually built as overhung. In order to avoid excessive overhang and unnecessary increase of the furnace chamber size, rotor wheels are fitted close to the chamber wall. This is also the reason for insufficient space for the stationary airfoils, which, in turn, considerably affects the efficiency and flow parameters of the axial blower. Therefore, the parameters of such blowers do not usually exceed the value of pressure difference ⁇ equalling 0.2 and the value of flow ⁇ equalling 0.3.
  • the invented blower particularly the one to be fitted in a chamber furnace, in the form of a rotor wheel with blades set diagonally on the shaft, set in an enclosure creating an inlet confuser duct, with its bridge with an approximate angle of 90° behind the rotor wheel, which turns smoothly into a radial diffuser, behind which it has a bridge shaped with an approximate angle of 90° ending with a nozzle box with nozzles
  • the hub of the rotor wheel has the shape of a solid of revolution with its slant height described by n degree polynomial and its Dp 2 outlet diameter greater than Dp 1 inlet diameter and the outward diameter of the axial and radial rotor wheel with spatially shaped blades monotonically increasing towards the flow from D 1 z inlet diameter to D 2 z outlet diameter.
  • the presented solution owing to the shape of the rotor allowing the shaping of the first bridge with a large angle, will enable an increase in the circulation efficiency and, at the same time, maintain the required thermodynamic parameters.
  • FIG. 1 presents a cross-section of the blower on the plane passing through its longitudinal axis and bridge axis, whereas
  • FIG. 2 presents a cross-section of the hub and the blade of the rotor wheel.
  • the blower shaft 1 there is a diagonally set rotor wheel 3 with spatially shaped blades 4 .
  • the wheel 3 is set in the enclosure 5 , creating the inlet confuser duct 6 .
  • Behind the rotor wheel 3 the blower has a bridge 7 with an approximate angle of 90°, which turns smoothly into a radial diffuser 8 , behind which there is another bridge 9 with an approximate angle of 90°, ending with a nozzle box 10 with nozzles 11 .
  • the hub 12 of the rotor wheel 3 has the shape of a solid of revolution with its slant height described by n degree polynomial, with its Dp 2 outlet diameter greater than Dp 1 inlet diameter and the outward diameter of the axial and radial rotor wheel 3 with spatially shaped blades 4 , monotonically increasing towards the flow from D 1 z inlet diameter to D 2 z outlet diameter.
  • the rotor wheel 3 is a semi-open wheel without a cover. Between the external contours of the blades 4 and the stationary body of the blower there is gap ⁇ , the size of which depends on mutual thermal dilatation of the wheel 3 and the body. It is also possible to deliver a blower, in which the wheel structure 3 is equipped with a cover.
  • the hot air or other gas flows through the stationary duct 6 , gaining acceleration of several percent, which favours levelling of the velocity profile on the inlet surface of the rotor wheel 3 .
  • the direction of the flow of the agent onto the blades 4 of the rotor wheel 3 is approximately axial.
  • the agent flows through the system of blades 4 of the rotor wheel 3 , which conveys energy to the agent in accordance with the basic equation for fluid flow machines (Euler's identity).
  • the agent is subject to compression.
  • the degree of compression depends upon a selection of geometrical parameters of the rotor wheel 3 and its rotating velocity.
  • the agent leaves the rotor wheel 3 at an angle in relation to the rotor rotation axis 3 —diagonally.
  • the ⁇ flow-out angle on the meridional plane is described by ⁇ relation ⁇ 90°.
  • the flow-out angle for the agent leaving the rotor wheel 3 depends on the assumed angle of the blade at the outlet and assumed rotating velocity.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The blower designed particularly for fitting in a chamber furnace has the hub of the rotor wheel in the shape of a solid of revolution with its slant height described by n degree polynomial and its Dp2 outlet diameter greater than Dp1 inlet diameter and the outward diameter of the axial and radial rotor wheel with spatially shaped blades monotonically increasing towards the flow from D1 z inlet diameter to D2 z outlet diameter.

Description

  • This invention relates to a blower designed for fitting in a chamber furnace in particular and used, among others, in furnaces for annealing of aluminium sheet.
  • In furnaces requiring circulation of hot gases, usually radial or axial blowers are used. The fitting of the latter is subject to significant restrictions that affect their operating parameters. Due to the conditions of the bearings operation, the blowers are usually built as overhung. In order to avoid excessive overhang and unnecessary increase of the furnace chamber size, rotor wheels are fitted close to the chamber wall. This is also the reason for insufficient space for the stationary airfoils, which, in turn, considerably affects the efficiency and flow parameters of the axial blower. Therefore, the parameters of such blowers do not usually exceed the value of pressure difference Ψ equalling 0.2 and the value of flow ψ equalling 0.3.
  • As compared to axial blowers, radial blowers used in furnaces ensure considerably greater pressure increments (with Ψ pressure difference exceeding 0.4) however they are burdened with significant defects. First of all, in order to achieve the required pressure increment, the dynamic pressure should be recovered in a reasonably efficient manner. In classic designs of blowers this is done in cumulative spirals with large angles of wrap, i.e. up to 360°. In chamber furnaces, air exhausted from the blower must go in two opposite ways. The use of one or two exhaust spirals is very difficult for structural reasons. In practice this results in an unequal distribution of velocities on both exhaust surfaces of the blower, which is even magnified by existence of a considerable angular momentum of the agent behind the rotor wheel. Such defects are typical of radial and drum blowers.
  • The description of the patent No. DE 10022788 presents a solution involving a use of an axial rotor with a constant outward diameter cooperating with two flat diffusers turning into two nozzle boxes. This blower is characterised by the same flow parameters as typical axial blowers, however, it shows much greater pressure increments and ensures an equal flow of the agent in both ways. Additionally, such blowers do not require using additional stators for the purposes of levelling of the field of velocity. However, the circulation efficiency of such blowers is relatively low (0.4). One of the reasons for such a low circulation efficiency is the fact that the agent leaving the axial rotor has a great kinetic energy and, therefore, losses generated in the bridge at the angle of 90° are also considerable, as diffusers operate with a rotational stall at the outlet.
  • The invented blower, particularly the one to be fitted in a chamber furnace, in the form of a rotor wheel with blades set diagonally on the shaft, set in an enclosure creating an inlet confuser duct, with its bridge with an approximate angle of 90° behind the rotor wheel, which turns smoothly into a radial diffuser, behind which it has a bridge shaped with an approximate angle of 90° ending with a nozzle box with nozzles is characterised in that the hub of the rotor wheel has the shape of a solid of revolution with its slant height described by n degree polynomial and its Dp2 outlet diameter greater than Dp1 inlet diameter and the outward diameter of the axial and radial rotor wheel with spatially shaped blades monotonically increasing towards the flow from D1 z inlet diameter to D2 z outlet diameter.
  • The presented solution, owing to the shape of the rotor allowing the shaping of the first bridge with a large angle, will enable an increase in the circulation efficiency and, at the same time, maintain the required thermodynamic parameters.
  • BRIEF DESCRIPTION OF DRAWINGS
  • The invention will be shown on an exemplary drawing, which does not restrict its construction as shown in the drawing, in which FIG. 1 presents a cross-section of the blower on the plane passing through its longitudinal axis and bridge axis, whereas
  • FIG. 2 presents a cross-section of the hub and the blade of the rotor wheel.
  • On the blower shaft 1 there is a diagonally set rotor wheel 3 with spatially shaped blades 4. The wheel 3 is set in the enclosure 5, creating the inlet confuser duct 6. Behind the rotor wheel 3 the blower has a bridge 7 with an approximate angle of 90°, which turns smoothly into a radial diffuser 8, behind which there is another bridge 9 with an approximate angle of 90°, ending with a nozzle box 10 with nozzles 11. The hub 12 of the rotor wheel 3 has the shape of a solid of revolution with its slant height described by n degree polynomial, with its Dp2 outlet diameter greater than Dp1 inlet diameter and the outward diameter of the axial and radial rotor wheel 3 with spatially shaped blades 4, monotonically increasing towards the flow from D1 z inlet diameter to D2 z outlet diameter. The rotor wheel 3 is a semi-open wheel without a cover. Between the external contours of the blades 4 and the stationary body of the blower there is gap δ, the size of which depends on mutual thermal dilatation of the wheel 3 and the body. It is also possible to deliver a blower, in which the wheel structure 3 is equipped with a cover.
  • The hot air or other gas flows through the stationary duct 6, gaining acceleration of several percent, which favours levelling of the velocity profile on the inlet surface of the rotor wheel 3. The direction of the flow of the agent onto the blades 4 of the rotor wheel 3 is approximately axial. Next, the agent flows through the system of blades 4 of the rotor wheel 3, which conveys energy to the agent in accordance with the basic equation for fluid flow machines (Euler's identity). The agent is subject to compression. The degree of compression depends upon a selection of geometrical parameters of the rotor wheel 3 and its rotating velocity. The agent leaves the rotor wheel 3 at an angle in relation to the rotor rotation axis 3—diagonally. The γ flow-out angle on the meridional plane is described by γ relation <90°. The flow-out angle for the agent leaving the rotor wheel 3 depends on the assumed angle of the blade at the outlet and assumed rotating velocity.

Claims (1)

1. The blower designed particularly for fitting in a chamber furnace, in the form of a rotor wheel with blades set diagonally on the shaft, set in an enclosure creating an inlet confuser duct, with its bridge with an approximate angle of 90° behind the rotor wheel, which turns smoothly into a radial diffuser, behind which it has a bridge shaped with an approximate angle of 90° ending with a nozzle box with nozzles wherein the hub of the rotor wheel has the shape of a solid of revolution with its slant height described by n degree polynomial and its Dp2 outlet diameter greater than Dp1 inlet diameter and the outward diameter of the axial and radial rotor wheel with spatially shaped blades monotonically increasing towards the flow from D1 z inlet diameter to D2 z outlet diameter.
US12/662,146 2010-04-01 2010-04-01 Blower designed for fitting particularly in a chamber furnace Abandoned US20110243728A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US12/662,146 US20110243728A1 (en) 2010-04-01 2010-04-01 Blower designed for fitting particularly in a chamber furnace

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/662,146 US20110243728A1 (en) 2010-04-01 2010-04-01 Blower designed for fitting particularly in a chamber furnace

Publications (1)

Publication Number Publication Date
US20110243728A1 true US20110243728A1 (en) 2011-10-06

Family

ID=44709891

Family Applications (1)

Application Number Title Priority Date Filing Date
US12/662,146 Abandoned US20110243728A1 (en) 2010-04-01 2010-04-01 Blower designed for fitting particularly in a chamber furnace

Country Status (1)

Country Link
US (1) US20110243728A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109214141A (en) * 2018-11-20 2019-01-15 西华大学 Rotating stall prediction method and device

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3028140A (en) * 1957-06-17 1962-04-03 James R Lage Rotary fluid flow machine having rotor vanes constructed according to three dimensional calculations
US3904308A (en) * 1973-05-16 1975-09-09 Onera (Off Nat Aerospatiale) Supersonic centrifugal compressors
DE10022788A1 (en) * 2000-05-10 2001-11-22 Ingenieurgemeinschaft Wsp Prof Hot gas ventilator for industrial oven; has semi-axial impeller enclosed directly by ninety degree deflector to guide volume flow from impeller radially away from impeller axis

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3028140A (en) * 1957-06-17 1962-04-03 James R Lage Rotary fluid flow machine having rotor vanes constructed according to three dimensional calculations
US3904308A (en) * 1973-05-16 1975-09-09 Onera (Off Nat Aerospatiale) Supersonic centrifugal compressors
DE10022788A1 (en) * 2000-05-10 2001-11-22 Ingenieurgemeinschaft Wsp Prof Hot gas ventilator for industrial oven; has semi-axial impeller enclosed directly by ninety degree deflector to guide volume flow from impeller radially away from impeller axis

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109214141A (en) * 2018-11-20 2019-01-15 西华大学 Rotating stall prediction method and device

Similar Documents

Publication Publication Date Title
US10731881B2 (en) Fan coil unit with shrouded fan
TWI726002B (en) Ventilation device
WO2016066112A1 (en) Centrifugal fan and air conditioner having same
EP3168481A1 (en) Propeller fan and blower unit
CN104350308B (en) There is axle and be placed in decelerator on axle, blower fan in fan shroud
US11542955B2 (en) Diagonal fan having an optimized diagonal impeller
CN203516203U (en) Centrifugal fan volute, centrifugal fan and sweeping machine
US10724538B2 (en) Centrifugal compressor
US20130022443A1 (en) Fan motor cooling
CN105102824B (en) Unilateral suction-type centrifugal blower
US10641284B2 (en) Centrifugal blower assemblies having a plurality of airflow guidance fins and method of assembling the same
JP6496010B2 (en) Apparatus and method for converting thermal energy
JP2009068372A (en) Centrifugal compressor
CN102852854A (en) Floor type air conditioner and oblique flow fan thereof
US10655471B2 (en) Turbine and gas turbine
US20110243728A1 (en) Blower designed for fitting particularly in a chamber furnace
WO2014122819A1 (en) Centrifugal compressor
WO2015198853A1 (en) Stator vane unit and steam turbine
EP2375079A1 (en) A blower designed for fitting particularly in a chamber furnace
CN202883468U (en) Floor-stand air conditioner and oblique flow fan thereof
CN204985067U (en) Fan and diffuser thereof
CN205779897U (en) Centrifugal fan
EP3686439B1 (en) Multi-stage centrifugal compressor
JP6402569B2 (en) Centrifugal compressor and centrifugal compressor design method
CN207018248U (en) A kind of Low-pressure axial fan impeller

Legal Events

Date Code Title Description
AS Assignment

Owner name: SECO/WARWICK S.A., POLAND

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MAGIERA, RADOMIR;KRYLLOWICZ, WLADYSLAW;JOZWIK, KRZYSZTOF;AND OTHERS;REEL/FRAME:026769/0001

Effective date: 20100401

Owner name: POLITECHNIKA LODZKA, POLAND

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:SECO/WARWICK S.A.;REEL/FRAME:026769/0051

Effective date: 20110601

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION